View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 51949U 22023D 24282.85801444 .00080266 00000-0 34575-2 0 9997
2 51949 63.4829 206.4052 0081533 339.0726 20.7055 15.19086418144136
| Epoch (UTC): | 08 October 2024 20:35:32 |
| Eccentricity: | 0.0081533 |
| inclination: | 63.4829° |
| perigee height: | 452 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 206.4052° |
| argument of perigee: | 339.0726° |
| revolutions per day: | 15.19086418 |
| mean anomaly at epoch: | 20.7055° |
| orbit number at epoch: | 14413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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